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1. 发明申请

US20080149760A1 Flight dynamics for an aircraft 有权
标题翻译：飞机的飞行动力学
公开(公告)号：US20080149760A1
公开(公告)日：2008-06-26
申请号：US11644712
申请日：2006-12-22
申请人： Clark M. Butler , Ian J. Gilchrist
发明人： Clark M. Butler , Ian J. Gilchrist
IPC分类号： B64D27/00
CPC分类号： B64D27/20 , B64D29/04
摘要： An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series Learjets are disclosed. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamic of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent the fuselage, wherein the new location is aft of the original location.
摘要翻译：一种包括机翼和挂架的飞机，其中塔架为机翼的翼型提供倒立的翼型，并且公开了用于改进20和30系列驾驶员的飞行动力学的改进和方法。改进包括机翼的前缘与飞行器的发动机的入口之间的距离增加，这减小了阻力并且增加了升高以提高飞行动力学的升力。塔的倒置翼型否定了塔架对飞行动力的影响，以改善飞机的整体飞行动态。该方法包括以下步骤：将原始发动机从原始塔架移除，从飞行器的机身移除原始塔架，并将新的塔架安装在与机身相邻的新位置，其中新的位置是原始位置的后方。

2. 发明申请

US20100237187A1 INVERTED AIRFOIL PYLON FOR AN AIRCRAFT 有权
标题翻译：用于飞机的倒装飞机飞轮
公开(公告)号：US20100237187A1
公开(公告)日：2010-09-23
申请号：US12789306
申请日：2010-05-27
申请人： Clark M. Butler , Ian J. Gilchrist
发明人： Clark M. Butler , Ian J. Gilchrist
IPC分类号： B64D27/00
CPC分类号： B64D27/20 , B64D29/04
摘要： An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series LEARJET® is provided. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the aircraft. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamics of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent to the fuselage, wherein the new location is aft of the original location.
摘要翻译：一种包括机翼和挂架的飞机，其中塔架为机翼的翼型提供倒立的翼型，并且提供了用于改进20和30系列LEARJET®的改进和改进的飞行动力学方法。该改进包括机翼的前缘与飞行器的发动机的入口之间的距离增加，这减少了阻力并增加了升高以提高飞机的飞行动态。塔的倒置翼型否定了吊架对飞行动态的影响，以改善飞机的整体飞行动力学。该方法包括以下步骤：将原始发动机从原始塔架移除，从飞机的机身移除原始塔架，以及将新的托架安装在与机身相邻的新位置，其中新位置在原始位置的后方。

3. 发明授权

US08376270B2 Structural dynamic stability for an aircraft 有权
标题翻译：飞机的结构动态稳定性
公开(公告)号：US08376270B2
公开(公告)日：2013-02-19
申请号：US13323471
申请日：2011-12-12
申请人： John Baker
发明人： John Baker
IPC分类号： B64C17/00 , B64C5/00
CPC分类号： B64C5/02 , B64C9/02
摘要： An improvement and method for improved structural dynamic stability for 20 and 30 Series Learjets are disclosed. The improvement includes a redistribution of the elevator mass balance to uncouple the elevator rotational motion from the stabilizer translation motion for the higher order horizontal frequencies having node lines in the proximity of the mass outboard counterbalance weights. The original tail section includes a rudder, and a horizontal stabilizer supporting an elevator mounted adjacent the rudder. The elevator includes a proximal end adjacent the rudder and a distal end that includes a counterbalance portion. The improvement includes replacement of an original mass counterbalance weight from within the counterbalance portion with a new mass counterbalance weight of less mass, and the inclusion of additional mass counterbalance weights disposed within the elevator and interposed between the proximal end and the counterbalance portion.
摘要翻译：公开了一种用于改进20和30系列LearJets的结构动态稳定性的改进和方法。改进包括电梯质量平衡的重新分配，以使电梯旋转运动与稳定器平移运动脱离，用于在质量外侧平衡重量附近具有节点线的较高阶水平频率。原始尾部包括方向舵和支撑安装在舵附近的电梯的水平稳定器。电梯包括邻近舵的近端和包括平衡部分的远端。该改进包括以较小质量的新的质量平衡重量从平衡部分内更换原始质量平衡重量，并且包括设置在电梯内并且插入在近端和平衡部分之间的附加质量平衡重。

4. 发明申请

US20120119019A1 Inverted Airfoil Pylon For An Aircraft 失效
标题翻译：飞机的倒立翼架
公开(公告)号：US20120119019A1
公开(公告)日：2012-05-17
申请号：US13346614
申请日：2012-01-09
申请人： Clark M. Butler , Ian J. Gilchrist
发明人： Clark M. Butler , Ian J. Gilchrist
IPC分类号： B64D27/02 , B64C1/38
CPC分类号： B64D27/20 , B64D29/04
摘要： An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series LEARJET® is provided. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the aircraft. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamics of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent to the fuselage, wherein the new location is aft of the original location.
摘要翻译：一种包括机翼和挂架的飞机，其中塔架为机翼的翼型提供倒立的翼型，并且提供了用于改进20和30系列LEARJET®的改进和改进的飞行动力学方法。该改进包括机翼的前缘与飞行器的发动机的入口之间的距离增加，这减少了阻力并增加了升高以提高飞机的飞行动态。塔的倒置翼型否定了吊架对飞行动态的影响，以改善飞机的整体飞行动力学。该方法包括以下步骤：将原始发动机从原始塔架移除，从飞机的机身移除原始塔架，以及将新的托架安装在与机身相邻的新位置，其中新位置在原始位置的后方。

5. 发明授权

US07770841B2 Inverted airfoil pylon for an aircraft 有权
标题翻译：飞机的倒立翼面塔
公开(公告)号：US07770841B2
公开(公告)日：2010-08-10
申请号：US11644712
申请日：2006-12-22
申请人： Clark M. Butler , Ian J. Gilchrist
发明人： Clark M. Butler , Ian J. Gilchrist
IPC分类号： B64D27/00
CPC分类号： B64D27/20 , B64D29/04
摘要： An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series LEARJET® is provided. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the aircraft. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamics of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent to the fuselage, wherein the new location is aft of the original location.
摘要翻译：一种包括机翼和挂架的飞机，其中塔架为机翼的翼型提供倒立的翼型，并且提供了用于改进20和30系列LEARJET®的改进和改进的飞行动力学方法。该改进包括机翼的前缘与飞行器的发动机的入口之间的距离增加，这减少了阻力并增加了升高以提高飞机的飞行动态。塔的倒置翼型否定了吊架对飞行动态的影响，以改善飞机的整体飞行动力学。该方法包括以下步骤：将原始发动机从原始塔架移除，从飞机的机身移除原始塔架，以及将新的托架安装在与机身相邻的新位置，其中新位置在原始位置的后方。

6. 发明申请

US20080149762A1 Structural dynamic stability for an aircraft 有权
标题翻译：飞机的结构动态稳定性
公开(公告)号：US20080149762A1
公开(公告)日：2008-06-26
申请号：US11644853
申请日：2006-12-22
申请人： John Baker
发明人： John Baker
IPC分类号： B64C9/02
CPC分类号： B64C5/02 , B64C9/02
摘要： An improvement and method for improved structural dynamic stability for 20 and 30 Series Learjets are disclosed. The improvement includes a redistribution of the elevator mass balance to uncouple the elevator rotational motion from the stabilizer translation motion for the higher order horizontal frequencies having node lines in the proximity of the mass outboard counterbalance weights. The original tail section includes a rudder, and a horizontal stabilizer supporting an elevator mounted adjacent the rudder. The elevator includes a proximal end adjacent the rudder and a distal end that includes a counterbalance portion. The improvement includes replacement of an original mass counterbalance weight from within the counterbalance portion with a new mass counterbalance weight of less mass, and the inclusion of additional mass counterbalance weights disposed within the elevator and interposed between the proximal end and the counterbalance portion.
摘要翻译：公开了一种用于改进20和30系列LearJets的结构动态稳定性的改进和方法。改进包括电梯质量平衡的重新分配，以使电梯旋转运动与稳定器平移运动脱离，用于在质量外侧平衡重量附近具有节点线的较高阶水平频率。原始尾部包括方向舵和支撑安装在舵附近的电梯的水平稳定器。电梯包括邻近舵的近端和包括平衡部分的远端。该改进包括以较小质量的新的质量平衡重量从平衡部分内更换原始质量平衡重量，并且包括设置在电梯内并且插入在近端和平衡部分之间的附加质量平衡重。

7. 发明授权

US08632032B2 Inverted airfoil pylon for an aircraft 失效
标题翻译：飞机的倒立翼面塔
公开(公告)号：US08632032B2
公开(公告)日：2014-01-21
申请号：US13346614
申请日：2012-01-09
申请人： Clark M. Butler , Ian J. Gilchrist
发明人： Clark M. Butler , Ian J. Gilchrist
IPC分类号： B64D27/14
CPC分类号： B64D27/20 , B64D29/04
摘要： An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series LEARJET® is provided. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the aircraft. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamics of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent to the fuselage, wherein the new location is aft of the original location.
摘要翻译：一种包括机翼和挂架的飞机，其中塔架为机翼的翼型提供倒立的翼型，并且提供了用于改进20和30系列LEARJET®的改进和改进的飞行动力学方法。该改进包括机翼的前缘与飞行器的发动机的入口之间的距离增加，这减少了阻力并增加了升高以提高飞机的飞行动态。塔的倒置翼型否定了吊架对飞行动态的影响，以改善飞机的整体飞行动力学。该方法包括以下步骤：将原始发动机从原始塔架移除，从飞机的机身移除原始塔架，以及将新的托架安装在与机身相邻的新位置，其中新位置在原始位置的后方。

8. 发明申请

US20120091268A1 Structural Dynamic Stability For An Aircraft 有权
标题翻译：飞机的结构动态稳定性
公开(公告)号：US20120091268A1
公开(公告)日：2012-04-19
申请号：US13323471
申请日：2011-12-12
申请人： John Baker
发明人： John Baker
IPC分类号： B64C9/30
CPC分类号： B64C5/02 , B64C9/02
摘要： An improvement and method for improved structural dynamic stability for 20 and 30 Series Learjets are disclosed. The improvement includes a redistribution of the elevator mass balance to uncouple the elevator rotational motion from the stabilizer translation motion for the higher order horizontal frequencies having node lines in the proximity of the mass outboard counterbalance weights. The original tail section includes a rudder, and a horizontal stabilizer supporting an elevator mounted adjacent the rudder. The elevator includes a proximal end adjacent the rudder and a distal end that includes a counterbalance portion. The improvement includes replacement of an original mass counterbalance weight from within the counterbalance portion with a new mass counterbalance weight of less mass, and the inclusion of additional mass counterbalance weights disposed within the elevator and interposed between the proximal end and the counterbalance portion.
摘要翻译：公开了一种用于改进20和30系列LearJets的结构动态稳定性的改进和方法。改进包括电梯质量平衡的重新分配，以使电梯旋转运动与稳定器平移运动脱离，用于在质量外侧平衡重量附近具有节点线的较高阶水平频率。原始尾部包括方向舵和支撑安装在舵附近的电梯的水平稳定器。电梯包括邻近舵的近端和包括平衡部分的远端。该改进包括以较小质量的新的质量平衡重量从平衡部分内更换原始质量平衡重量，并且包括设置在电梯内并且插入在近端和平衡部分之间的附加质量平衡重。

9. 发明授权

US08091824B2 Inverted airfoil pylon for an aircraft 有权
标题翻译：飞机的倒立翼面塔
公开(公告)号：US08091824B2
公开(公告)日：2012-01-10
申请号：US12789306
申请日：2010-05-27
申请人： Clark M. Butler , Ian J. Gilchrist
发明人： Clark M. Butler , Ian J. Gilchrist
IPC分类号： B64D27/14
CPC分类号： B64D27/20 , B64D29/04
摘要： An aircraft including a wing and a pylon, wherein the pylon provides an airfoil inverted for an airfoil of the wing, and an improvement and method for improved flight dynamics for 20 and 30 Series LEARJET® is provided. The improvement includes an increased distance between a leading edge of a wing and an intake of an engine of the aircraft, which reduces drag and increases lift for improved flight dynamics of the aircraft. The inverted airfoil of the pylon negates an influence of the pylon on flight dynamics for improved overall flight dynamics of the aircraft. The method includes steps of removing an original engine from an original pylon, removing the original pylon from the fuselage of the aircraft, and mounting a new pylon in a new location adjacent to the fuselage, wherein the new location is aft of the original location.
摘要翻译：一种包括机翼和挂架的飞机，其中塔架为机翼的翼型提供倒立的翼型，并且提供了用于改进20和30系列LEARJET®的改进和改进的飞行动力学方法。该改进包括机翼的前缘与飞行器的发动机的入口之间的距离增加，这减少了阻力并增加了升高以提高飞机的飞行动态。塔的倒置翼型否定了吊架对飞行动态的影响，以改善飞机的整体飞行动力学。该方法包括以下步骤：将原始发动机从原始塔架移除，从飞机的机身移除原始塔架，以及将新的托架安装在与机身相邻的新位置，其中新位置在原始位置的后方。

10. 发明授权

US08074926B2 Structural dynamic stability for an aircraft 有权
标题翻译：飞机的结构动态稳定性
公开(公告)号：US08074926B2
公开(公告)日：2011-12-13
申请号：US11644853
申请日：2006-12-22
申请人： John Baker
发明人： John Baker
IPC分类号： B64C17/00
CPC分类号： B64C5/02 , B64C9/02
摘要： An improvement and method for improved structural dynamic stability for 20 and 30 Series Learjets are disclosed. The improvement includes a redistribution of the elevator mass balance to uncouple the elevator rotational motion from the stabilizer translation motion for the higher order horizontal frequencies having node lines in the proximity of the mass outboard counterbalance weights. The original tail section includes a rudder, and a horizontal stabilizer supporting an elevator mounted adjacent the rudder. The elevator includes a proximal end adjacent the rudder and a distal end that includes a counterbalance portion. The improvement includes replacement of an original mass counterbalance weight from within the counterbalance portion with a new mass counterbalance weight of less mass, and the inclusion of additional mass counterbalance weights disposed within the elevator and interposed between the proximal end and the counterbalance portion.
摘要翻译：公开了一种用于改进20和30系列LearJets的结构动态稳定性的改进和方法。改进包括电梯质量平衡的重新分配，以使电梯旋转运动与稳定器平移运动脱离，用于在质量外侧平衡重量附近具有节点线的较高阶水平频率。原始尾部包括方向舵和支撑安装在舵附近的电梯的水平稳定器。电梯包括邻近舵的近端和包括平衡部分的远端。该改进包括以较小质量的新的质量平衡重量从平衡部分内更换原始质量平衡重量，并且包括设置在电梯内并且插入在近端和平衡部分之间的附加质量平衡重。

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